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Flight Instructors Training Procedures _revised AIC_x

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2. SIDE SLIP WHILE TURNING – SLIPPING<br />

TURNS<br />

i. Establish the aircraft in a normal gliding turn<br />

without flaps then enter a slipping turn.<br />

3. SIDESLIP WHILE MANTAINING TRACK –<br />

NOSE STRAIGHT<br />

i. To be demonstrated from a normal power off<br />

glide or from a power-assisted descent in a<br />

crosswind condition.<br />

the aircraft laterally, whilst using the<br />

elevators to maintain the normal<br />

straight glide nose attitude.<br />

b. Note that the normal indicated glide<br />

speed is regained, because the correct<br />

gliding attitude has been maintained.<br />

Note loss of height during side slip.<br />

c. Engine considerations.<br />

i. Look out.<br />

ii. Engine considerations.<br />

iii. Note the rate of descent.<br />

iv. Note the IAS/nose attitude relationship.<br />

v. Entry:<br />

a. Apply aileron in the direction of the<br />

bank.<br />

b. Simultaneously, apply sufficient top<br />

rudder to prevent the nose from yawing<br />

too rapidly towards the lower wing, in<br />

addition also preventing an increase in<br />

the rate of turn.<br />

c. Maintain the gliding turn attitude.<br />

vi. During the slipping.<br />

a. Regulate the rate of turn with ailerons<br />

and rudder.<br />

b. Maintain required nose attitude.<br />

c. Note:<br />

i. Higher rate of descent .<br />

ii. IAS/nose attitude relationship.<br />

iii. Positive application of flight<br />

control required.<br />

vii. Recovery from the slipping turn:<br />

a. Simultaneously and smoothly reduce<br />

rudder and aileron application until the<br />

balanced gliding turn is regained.<br />

b. Note normal indicated gliding speed<br />

regained.<br />

c. Engine considerations.<br />

i Look out.<br />

ii Engine considerations.<br />

iii Select a line feature with the wind blowing<br />

across it and align the aircraft with this<br />

feature.<br />

iv Entry:<br />

a. Slowly apply ailerons into wind<br />

simultaneously applying sufficient<br />

opposite rudder (top rudder) to prevent<br />

the aircraft nose from yawing away<br />

from the line feature.<br />

b. Maintain the desired attitude with the<br />

elevators – note the IAS error is now<br />

negligible.<br />

!"#$ # &"" '$ #

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